View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 49294U 26145.33428837 +.00000000 +00000-0 +29052-3 0 00008
2 49294 87.9164 279.0094 0002112 79.7024 280.4347 13.20772148 04
| Epoch (UTC): | 25 May 2026 08:01:22 |
| Eccentricity: | 0.0002112 |
| inclination: | 87.9164° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 279.0094° |
| argument of perigee: | 79.7024° |
| revolutions per day: | 13.20772148 |
| mean anomaly at epoch: | 280.4347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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